A particulate filtration reverse pulse cleaning system is disclosed. The system comprising a housing, a tubesheet disposed within the housing, a filter for fluid communication with a tubesheet aperture, a support frame connectable with the tubesheet, and a cleaning system associated with the support frame. A filter cleaning system is also disclosed, the support frame comprising a plurality of hollow support legs comprising at least one cleaning aperture and a cleaning system associated with the plurality of hollow support legs. A method for cleaning a filter is also disclosed.
|
1. A particulate filtration reverse pulse cleaning system comprising:
a housing through which air flows in a first direction towards a housing outlet;
a tubesheet disposed within the housing, the tubesheet comprising a tubesheet aperture;
a filter for fluid communication with the tubesheet aperture, the filter comprising an open end adapted to be located adjacent to and surrounding the tubesheet aperture;
a support frame connectable with the tubesheet, the support frame supporting the filter, the filter through which air flows in the first direction, the support frame including a plurality of hollow support legs; and
a cleaning system associated with the support frame, the cleaning system comprising a cleaning jet source directing cleaning fluid through at least one of the plurality of hollow support legs in a second direction opposite the first direction, the cleaning jet source comprising a plurality of cleaning jet sources located along the length of the plurality of support legs, wherein the plurality of the support legs are approximately equally radially spaced from each other about a circumference of the tubesheet aperture, and the plurality of support legs comprise three support legs in a tripod configuration.
2. The system of
3. The system of
5. The system of
an end plate disposed upon a first closed end of the filter on a first plenum side of the housing, the end plate coupled to the plurality of support legs via a carriage bolt.
6. The system of
7. The system of
8. The system of
9. The system of
10. The system of
|
The present invention generally relates to the removal of particulate matter from a filter media. More specifically, embodiments of the present invention relate to a reverse pulse integrated cleaning system for removing particulate matter from a fabric filter media.
Industrial gas turbine applications utilize intake air during normal operation for combustion purposes. The intake air is drawn through the compressor where it is subsequently mixed with fuel and ignited in a combustor, providing the driving force for a turbine. Because gas turbines are essentially air breathing engines, many factors and characteristics of intake air can affect performance and overall efficiency of a gas turbine system.
Factors that may affect the performance and efficiency of a gas turbine include the temperature of the intake air, site elevation, humidity, and the presence of contaminants in the intake air flow. The presence of contaminants in particular, has a significant detrimental impact on turbine efficiency. Contaminants such as dirt, dust, and salt can cause compressor blade corrosion, erosion, and fouling where the resulting surface roughness decreases compressor air flow and efficiency. This in turn, reduces the gas turbine output and overall thermal efficiency of the system.
In order to combat the effect of contaminants on gas turbine efficiency, filtration systems are typically used to remove particulate matter from an intake air stream. These systems may feature a filter media on the upstream side of a compressor in order to capture particulate matter before it reaches the combustor. Although effective, during long periods of operation, the filter media may become saturated with particulate matter, which subsequently impedes the flow of air and creates a significant pressure drop between the upstream and downstream side of the filter media. Therefore, periodic cleaning of the filter may be necessary.
Reverse pulse cleaning systems are known in the art for removing particulate matter from saturated filter media. These systems typically have a nozzle downstream of the filter connected to an air supply, where cleaning air is provided by the air supply and directed into the filter via the nozzle in a direction opposite of intake air flow. Because obtaining uniform cleaning down the length of the filter media provides enhanced gas turbine efficiency, an apparatus that accomplishes that goal may be desirable.
One embodiment of the present invention is a particulate filtration reverse pulse cleaning system comprising a housing through which air flows in a first direction towards a housing outlet. A tubesheet is disposed within the housing, the tubesheet comprising a tubesheet aperture. There is also a filter for fluid communication with the tubesheet aperture, the filter comprising an open end adapted to be located adjacent to and surrounding the tubesheet aperture. There is a support frame connectable with the tubesheet, the support frame for supporting the filter, the filter through which air flows in the first direction, and the support frame comprising a plurality of support legs. Finally, there is a cleaning system associated with the support frame, the cleaning system comprising a cleaning jet source associated with the plurality of support legs for directing cleaning fluid in a second direction opposite the first direction.
In another embodiment of the present invention, there is a filter cleaning system comprising a support frame comprising a plurality of hollow support legs comprising at least one cleaning aperture. There is also a cleaning system associated with the plurality of hollow support legs, the cleaning system for directing cleaning fluid in a second direction through the at least one cleaning aperture.
A method for cleaning a filter is disclosed, the method comprising providing a support frame comprising a plurality of support legs, a filter, and a cleaning system associated with the support frame. The cleaning system also comprising a cleaning jet source for directing cleaning fluid in a second direction. The method also further comprising positioning the filter around the support frame and providing cleaning fluid to the cleaning system at a supply pressure sufficient to dislodge particulate matter from the filter.
Further features of the invention will become apparent to those skilled in the art to which the invention relates from reading the following description with reference to the accompanying drawings, in which:
Embodiments of the present invention are directed to the use of an integrated reverse pulse cleaning system for gas turbine inlet filters, featuring a support frame for facilitating improved cleaning efficiency, elongated filter life span, and prevention of filter oscillations and air bypass.
For the entirety of this document, “fluid” shall include, but is not limited to, air or any other suitable medium for facilitating cleaning of a filter media. “Substantially unimpeded flow” shall mean the ability of fluid to flow between destinations without experiencing a pressure drop.
Horizontally or vertically arranged filter cartridges that collect and prevent particulate matter from entering a gas turbine system are typically held in place by a multi-legged support frame. In these systems, the support frame is coupled to a tubesheet and a filter cartridge and arranged such that an open end of the filter is secured to the tubesheet. In these arrangements, particulate matter is removed from the filter media via an air pulse nozzle located downstream of a filter cartridge. However, as the distance between the air pulse nozzle and areas of the filter increase, cleaning efficiency may suffer. Therefore, one aspect of the invention provides a support frame including an integrated cleaning system to overcome the consequences of previously known downstream reverse pulse cleaning systems.
As shown in
The air filter unit 1 may include a housing 7 which may be of any suitable configuration to allow the encapsulation of a tubesheet 11 and any desired amount of filters 9 for effective filtration and sufficient air flow to the gas turbine unit 3. The housing 7 may be several stories high and contain up to several hundred filters 9. As shown in
The tubesheet 11 may be constructed and arranged to separate the housing 7 into a first plenum side of the housing which is located upstream of the filter 9 and a second plenum side which is located downstream of the filter 9. Tubesheet 11 may be a vertical sheet constructed of any material suitable for preventing the passage of air therethrough.
The filter 9 may be any suitable configuration and material to allow the collection of particulate matter on its surface. Filter 9 may be secured to the tubesheet through any suitable means, where in exemplary embodiments, a support frame (not shown) may be connectable with the tubesheet 11 for supporting the filter 9. Filter 9 may be a fabric filter media, specifically constructed and configured for facilitating the collection of particulate matter.
Referring now to
As mentioned above, the support frame 25 may include any desired number of support legs. The support legs may facilitate substantially uniform cleaning of the filter 9. In exemplary embodiments of the present invention, the support legs may be approximately equally radially spaced from each other about a circumference of the tubesheet aperture 41. For example, if the support frame 25 includes three support legs in a tripod configuration, each leg may be spaced at approximately 120° from each other.
Furthermore, in reference to
Also as shown in
As mentioned above,
In order to facilitate fluid communication, such as, but not limited to, substantially unimpeded flow, between the cleaning aperture, support legs that may be hollow, and the pulse tube, many configurations may be utilized. One possible configuration, as shown in
Another configuration for facilitating fluid communication, such as, but not limited to, substantially unimpeded flow, is shown in
Cleaning fluid may be supplied to the support frame 25 for any suitable duration and at any pressure necessary for cleaning the filter 9. However, it may be desirable for cleaning fluid to not be supplied in such a way that cleaning fluid flowing in a second direction F2 is not greater than the flow of intake air in a first direction. It is desirable to perform reverse pulse cleaning without impeding the flow of intake air and operation of the power generation unit. Therefore, in an exemplary embodiment, cleaning fluid may be supplied to the cleaning system at a pressure in the range of about 5 bar to about 8 bar and for a duration in the range of about 0.05 seconds to about 0.5 seconds.
As shown in
A method for cleaning a filter is illustrated in
It will be understood that, although the terms first, second, etc. may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of example embodiments. As used herein, the term “and/or” includes any, and all, combinations of one or more of the associated listed items.
The terminology used herein is for describing particular embodiments only and is not intended to be limiting of example embodiments. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises”, “comprising”, “includes” and/or “including”, when used herein, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof.
From the above description of at least one aspect of the invention, those skilled in the art will perceive improvements, changes and modifications. Such improvements, changes and modifications within the skill of the art are intended to be covered by the appended claims.
Larcombe, Simon Charles, Jarrier, Etienne René
Patent | Priority | Assignee | Title |
11872576, | Feb 24 2020 | ALTAIR UK LIMITED | Pulse nozzle for filter cleaning systems |
8834591, | Oct 01 2010 | AAF-McQuay Inc. | Filter structure for removing contaminants from stream of fluid |
9415340, | Oct 01 2010 | American Air Filter Company Inc. | Filter structure for removing contaminants from stream of fluid |
Patent | Priority | Assignee | Title |
4058379, | May 27 1975 | Phillips Petroleum Company | Filtering apparatus |
4147522, | Apr 23 1976 | AMERICAN PRECISION INDUSTRIES INC , A DE CORP | Electrostatic dust collector |
4171963, | Feb 01 1978 | Donaldson Company, Inc. | Filter element support member |
4209310, | Jul 05 1974 | Donaldson Company, Inc. | Filter element mounting mechanism |
4278454, | May 29 1979 | VENTUREDYNE, LTD A WISCONSIN CORP | Filter apparatus with reverse flow cleaning |
4336035, | Mar 12 1979 | Wheelabrator-Frye Inc. | Dust collector and filter bags therefor |
4357151, | Feb 25 1981 | American Precision Industries Inc. | Electrostatically augmented cartridge type dust collector and method |
4544389, | Nov 07 1983 | Multiple jet backflushed air filter | |
4578092, | Nov 04 1983 | VENTUREDYNE, LTD A WISCONSIN CORP | Method and apparatus for improving the operation of a dust collector |
4735638, | Nov 18 1986 | UNITED STATES OF AMERICA, THE, AS REPRESENTED BY THE DEPARTMENT OF ENERGY | Filter unit for use at high temperatures |
4738696, | Jul 16 1987 | Baghouse installations | |
4820320, | Feb 16 1988 | Compact dust collector | |
4867771, | Jul 12 1984 | BHA GROUP HOLDINGS, INC | Tensioning device for bag filters |
6875256, | Sep 05 2000 | Donaldson Company, Inc. | Methods for filtering air for a gas turbine system |
8114196, | Aug 31 2009 | BHA Altair, LLC | Gas turbine inlet filter house cleaning apparatus and method |
20020073849, | |||
20080022855, | |||
20090107337, | |||
20100326024, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
May 12 2010 | JARRIER, ETIENNE RENE | General Electric Company | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 024580 | /0535 | |
May 12 2010 | LARCOMBE, SIMON CHARLES | General Electric Company | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 024580 | /0535 | |
Jun 23 2010 | General Electric Company | (assignment on the face of the patent) | / | |||
Dec 16 2013 | General Electric Company | BHA Altair, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 031911 | /0797 | |
Dec 16 2013 | BHA Group, Inc | BHA Altair, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 031911 | /0797 | |
Dec 16 2013 | ALTAIR FILTER TECHNOLOGY LIMITED | BHA Altair, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 031911 | /0797 | |
Dec 23 2020 | BHA Altair, LLC | Parker-Hannifin Corporation | MERGER SEE DOCUMENT FOR DETAILS | 060062 | /0932 | |
Jun 24 2022 | Parker-Hannifin Corporation | Parker Intangibles LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 060440 | /0130 |
Date | Maintenance Fee Events |
Apr 04 2014 | ASPN: Payor Number Assigned. |
Aug 26 2016 | M1551: Payment of Maintenance Fee, 4th Year, Large Entity. |
Aug 26 2020 | M1552: Payment of Maintenance Fee, 8th Year, Large Entity. |
Aug 26 2024 | M1553: Payment of Maintenance Fee, 12th Year, Large Entity. |
Date | Maintenance Schedule |
Feb 26 2016 | 4 years fee payment window open |
Aug 26 2016 | 6 months grace period start (w surcharge) |
Feb 26 2017 | patent expiry (for year 4) |
Feb 26 2019 | 2 years to revive unintentionally abandoned end. (for year 4) |
Feb 26 2020 | 8 years fee payment window open |
Aug 26 2020 | 6 months grace period start (w surcharge) |
Feb 26 2021 | patent expiry (for year 8) |
Feb 26 2023 | 2 years to revive unintentionally abandoned end. (for year 8) |
Feb 26 2024 | 12 years fee payment window open |
Aug 26 2024 | 6 months grace period start (w surcharge) |
Feb 26 2025 | patent expiry (for year 12) |
Feb 26 2027 | 2 years to revive unintentionally abandoned end. (for year 12) |